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Patent # Description
2016/0208675 COOLING SYSTEM, DEVICE AND METHOD FOR A VEHICLE
A cooling system includes a cooling loop containing a cooling fluid configured for circulation through an engine, an auxiliary alternator configured to be...
2016/0208674 FAN SHROUD FOR MOTOR VEHICLE
A fan shroud assembly for a vehicle including a fan shroud for the vehicle which minimizes a noise generated by utilizing additional or supplemental flow...
2016/0208673 SUPPORT RING FOR AN EXHAUST GAS DUCT SYSTEM
A support ring (36) for an exhaust gas duct system, especially of an internal combustion engine of a vehicle, comprises a support element body (40) with a...
2016/0208672 PRODUCING METHOD OF WOUND MUFFLER, AND WOUND MUFFLER
A muffler is a wound muffler formed by inserting a silencer into an inside of a main body formed in a cylindrical shape, the silencer includes an expandable...
2016/0208671 PROTECTIVE SHIELDS TO REDUCE EXHAUST SOOT AND CONDENSATE DEPOSITION
An exhaust assembly that includes an exhaust pipe extending rearward from a vehicle; and a bezel in close proximity with, or coupled to, a vehicle fascia, the...
2016/0208670 DEF INJECTOR COOLING SYSTEM AND METHOD
A DEF injector cooling system may include a mechanical pump, an electric pump, and a controller. The mechanical pump may be rotatably coupled to an engine so...
2016/0208669 SINGLE SENSOR MONITORING SYSTEM FOR MULTIPLE AFTER-TREATMENT SYSTEMS ON ENGINES
An aftertreatment system comprises a first passageway to receive a first portion and a second passageway to receive a second portion of the exhaust gas from...
2016/0208668 DIAGNOSTIC APPARATUS FOR EXHAUST GAS PURIFICATION APPARATUS (AS AMENDED)
A diagnostic apparatus for an exhaust gas purification apparatus including a selective catalytic reduction NOx catalyst (SCR catalyst) provided in an exhaust...
2016/0208667 ENGINE EMISSION ABSORBER ASSEMBLY AND METHOD FOR OPERATING SAME
An absorber assembly for an engine system and a method for operating the same is provided. The absorber assembly also includes a first section and a second...
2016/0208666 System And Method For Detecting Face-Plugging Of An Exhaust Aftertreatment Component
An exhaust aftertreatment system may include an oxidation catalyst, a soot sensor, a filter and a control module. The oxidation catalyst may be disposed in an...
2016/0208665 WORK VEHICLE
Regarding a work vehicle that includes an engine mounted on a travelling machine body and an exhaust gas purification device arranged in an exhaust gas path of...
2016/0208664 SYSTEM TO GENERATE PRESSURIZED AIR FOR HYDRO-EXCAVATION
A system to generate pressurized air for hydro-excavation includes an exhaust silencer configured to hold water and an exhaust manifold disposed through the...
2016/0208663 ENGINE OIL SUPPLY APPARATUS
An oil supply apparatus includes: an oil pump; a main oil supply path; a sub oil supply path connected to the main oil supply path; a first oil supply section...
2016/0208662 MULTI-LINK PISTON-CRANK MECHANISM FOR INTERNAL COMBUSTION ENGINE
When the compression ratio of a variable compression ratio internal combustion engine (10) is set at a low compression ratio, a lubricating oil ejected from a...
2016/0208661 VARIABLE VALVE APPARATUS FOR INTERNAL COMBUSTION ENGINE
An variable valve apparatus for an internal combustion engine according to the invention includes a cam base member, an elastic member, a cam lobe member, and...
2016/0208660 HYDRAULIC LASH ADJUSTER
The invention provides a hydraulic lash adjuster equipped with a cost effective dropout preventing mechanism for preventing a plunger from dropping out of a...
2016/0208659 REACTOR SYSTEM AND SOLID FUEL COMPOSITE THEREFOR
A reactor system includes a fluidized-bed. A fuel and a sulfur absorbent material are eluted through the fluidized-bed. The reactor system may include a heat...
2016/0208658 METHOD FOR THE RECOVERY OF PROCESS WASTEWATERS OF A FOSSIL-FUELED STEAM POWER PLANT AND FOSSIL-FUELED STEAM...
A fossil-fueled steam power plant and method, the plant has a water-steam circuit, cooling water circuit, flue gas cleaning system and cooling tower. A...
2016/0208657 OPERATING METHOD FOR STARTING A ONCE-THROUGH STEAM GENERATOR HEATED USING SOLAR THERMAL ENERGY
An operating method for starting a once-through steam generator heated using solar thermal energy, wherein a flow medium flowing through the once-through steam...
2016/0208656 OPERATING METHOD FOR AN EXTERNALLY HEATED FORCED-FLOW STEAM GENERATOR
An operating method for an externally heated once-through steam generator, in particular a once-through steam generator is heated using solar thermal energy...
2016/0208655 TIE ROD FOR A MID-TURBINE FRAME
A mid-turbine frame for a gas turbine engine includes an inner frame case that includes a bolt opening and at least one spoke for connecting an outer frame...
2016/0208654 A CASING STRUCTURE WITH CONNECTION TABS
A casing structure interposed between the engine and the nacelle of an aircraft, the casing structure including a shroud surrounding the engine and including a...
2016/0208653 CASING STRUCTURE INTERPOSED BETWEEN THE ENGINE AND THE NACELLE HAVING A MOUNTING PLATE WITH BOLTS
An aircraft casing structure including a shroud surrounding the engine and made up of a plurality of sectors; a plurality of radial arms, each mounted between...
2016/0208652 ENCLOSED JACKING INSERT
A case assembly is provided. The case assembly comprises a first flange and a spot face in the first flange. The spot face has a D-shaped perimeter. A jacking...
2016/0208651 CONTROLLING LUBRICANT FLOW IN EPICYCLIC GEARBOX
A disclosed lubrication system for a turbofan engine includes a pump for driving lubricant through a lubrication circuit, at least one sensor generating a...
2016/0208650 DEOILER DEBRIS BAFFLE
Aspects of the disclosure are directed to a system associated with an engine of an aircraft, comprising: a deoiler configured to receive a mixture of air and...
2016/0208649 WALL FOR A HOT GAS CHANNEL IN A GAS TURBINE
A wall for a hot gas channel in a gas turbine is described, the wall having a back side and a front side and an impingement sheet having impingement cooling...
2016/0208648 COOLING PASSAGES FOR A MID-TURBINE FRAME
A mid-turbine frame for a gas turbine engine includes at least one spoke for connecting an outer frame case to an inner frame case. At least one spoke includes...
2016/0208647 COOLING PASSAGES FOR A MID-TURBINE FRAME
A mid-turbine frame for a gas turbine engine includes an inner frame case that includes a fluid passage. A swirler tube is in fluid communication with the...
2016/0208646 COOLING PASSAGES FOR A MID-TURBINE FRAME
A mid-turbine frame for a gas turbine engine includes an outer frame case and an inner frame case. At least one spoke connects the outer frame case to the...
2016/0208645 BLADE OUTER AIR SEAL COOLING SCHEME
A cooling scheme for a blade outer air seal includes a perimeter cooling arrangement configured to convectively cool a perimeter of the blade outer air seal,...
2016/0208644 COOLING PASSAGES FOR A MID-TURBINE FRAME
A mid-turbine frame for a gas turbine engine includes an outer frame case and an inner frame case. At least one spoke connects the outer frame case to the...
2016/0208643 TURBOMACHINE FLOW PATH HAVING CIRCUMFERENTIALLY VARYING OUTER PERIPHERY
A turbomachine includes an annular flow path section between a plurality of radially extending stator vanes and a plurality of radially extending rotor blades....
2016/0208642 TURBINE EXHAUST CYLINDER/TURBINE EXHAUST MANIFOLD BOLTED FULL SPAN TURBINE EXHAUST FLAPS
A system and method to minimize flow induced vibration in a gas turbine exhaust is provided. The system includes a turbine exhaust manifold connected to a...
2016/0208641 TRANSLATING VARIABLE AREA FAN NOZZLE PROVIDING AN UPSTREAM BYPASS FLOW EXIT
A variable area fan nozzle assembly for a turbofan engine includes a nacelle having an aft edge and a translating nozzle segment having a forward edge and a...
2016/0208640 GAS TURBINE ENGINE
A fan containment system has a fan case having an annular casing element for encircling an array of fan blades and a hook projecting generally radially...
2016/0208639 SYSTEM AND METHOD FOR CONTROLLING A GAS TURBINE ENGINE
A control system for a gas turbine engine including a power turbine is disclosed. The control system may include a control module to receive engine operating...
2016/0208638 TURBINE DAMPING DEVICE
A turbine damping device is mounted on a fitness device, and has a housing assembly, a turbine assembly, and a regulating unit. The turbine assembly is mounted...
2016/0208637 VARIABLE VANE BUSHING
A variable vane assembly includes a variable vane, a trunnion arranged on one end of the variable vane, an inner bushing configured to receive the trunnion in...
2016/0208636 STEAM GOVERNING VALVE APPARATUS AND POWER GENERATION FACILITY
With a simple structure in which the component count is reduced, the occurrence of noise and vibrations can be prevented in a range from a minute opening...
2016/0208635 TURBINE SHROUD WITH TUBULAR RUNNER-LOCATING INSERTS
A turbine shroud for a gas turbine engine includes a carrier and a blade track. The blade track includes an annular runner and a plurality of inserts that...
2016/0208634 REPAIR OR REMANUFACTURE OF BLADE OUTER AIR SEALS FOR A GAS TURBINE ENGINE
A method of remanufacturing a turbine component is provided. This method includes removing a donor portion from a damaged component; removing a to-be-replaced...
2016/0208633 TURBINE SHROUD ASSEMBLY
A turbine shroud assembly includes a plurality of arcuate shroud block assemblies annularly arranged to form a shroud segment. The plurality of shroud block...
2016/0208632 SLIDING SEAL
The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a seal ring including a radially extending base...
2016/0208631 LEAKAGE AIR SYSTEMS FOR TURBOMACHINES
A cooling system for a turbomachine includes a vane having an outer diameter platform at one end and an inner diameter platform at another end opposite the...
2016/0208630 SEALING RING SEGMENT FOR A STATOR OF A TURBINE
A sealing ring segment for a stator of a turbine, the sealing ring segment has substantially the shape of a cylinder casing segment and has on its outer side a...
2016/0208629 ANTI-ROTATION VANE
A vane for a gas turbine engine includes a radially inner platform and a radially outer platform. At least two airfoils extend between the radially inner...
2016/0208628 INNER HOUSING HUB FOR A GAS TURBINE
An inner housing hub is arranged in a gas turbine about a gas turbine shaft and is formed as a component of an inner housing used to deflect hot gases exiting...
2016/0208627 COOLING FEED ORIFICES
An airfoil platform includes a platform body having an arcuate base defining a centerline axis. A rail extends radially outboard from a side of the arcuate...
2016/0208626 INTEGRALLY BLADED ROTOR WITH PRESSURE SIDE THICKNESS ON BLADE TRAILING EDGE
An integrally bladed rotor comprises a hub centered about an axis and having a plurality of blades extending radially outwardly of the axis across a span. Each...
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